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Analysis of rubber forming process of fire barrier from titanium CP2 alloy for AW 139 helicopter

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Języki publikacji
EN
Abstrakty
EN
This paper presents conditions of forming products from titanium sheets by means of rubber stamping method. After introducing the issues connected with these elements manufacturing for aviation industry, considering standards and legal regulations, technological problems occurring during forming deep stiffening ribs. The results in the characteristic curvatures and distortion in the final products were generated in the process heterogeneous internal stress state. The Authors aimed at explaining and presenting of solutions limiting occurrence of chosen shape faults, which disqualify these products application in aviation industry. The proposed solutions significantly reduced the incidence of these unfavorable phenomena. The modified method of rubber stamping of firewall from titanium alloy CP-2 sheet was successfully implemented in manufacturing conditions of PZL Swidnik.
Słowa kluczowe
Twórcy
autor
  • The Communication Equipment Manufacturing „PZL-Świdnik” S.A., Lotników Polskich 1, 21-045 Świdnik, Poland
autor
  • Department of Computer Modelling and Metal Forming Technologies, Mechanical Engineering Faculty, Lublin University of Technology, 36 Nadbystrzycka Str., 20-618 Lublin, Poland
Bibliografia
  • 1. Tekkaya A.E., Taylan A. Sheet metal forming. Processes and applications. Materials Park, ASM International, Ohio 2012.
  • 2. Minghua Z., Qiang X.Y., Yu L., Wenliang C. Prediction algorithm of blank shape for rubber forming of aircraft sheet metal part. AIP Conference Proc. 22.8.2011, Vol. 1383, Iss. 1, 2011, 943–947.
  • 3. Vilcans J., Torims T. Thin sheet metal stamping with elastic media. Annals of DAAAM & Proc. of the 21st DAAAM Symposium, Croatia, Zadar, (20-23.10.2010), 2010, 849–850.
  • 4. Standards JAR/FAR 29.
  • 5. Company standard Agusta Westland No 999-0010-08.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-7bea9ccb-0c31-4ca6-bfb2-e416682db2ef
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